Resin composition for resin molding, and resin molding

ABSTRACT

A resin molding including a polyolefin, a polyamide in a content of 1 part by mass to 50 parts by mass per 100 parts of the polyolefin, carbon fibers in a content of 1 part by mass to 50 parts by mass per 100 parts by mass of the polyolefin, organic fibers in a content of 1 part by mass to 20 parts by mass per 100 parts by mass of the polyolefin, and a carboxylic anhydride-modified polyolefin as a compatibilizer in a content of 1 part by mass to 10 parts by mass per 100 parts by mass of the polyolefin, where a proportion of a carbon fiber and an organic fiber each having a fiber length in a range of 1 mm to 20 mm to all the carbon fibers and the organic fibers is 1% to 20% by number.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a Division of application Ser. No. 15/663,994 filedJul. 31, 2017, which in turn is allowed and claims priority to JapanesePatent Application No. 2017-058683 filed Mar. 24, 2017.

BACKGROUND Technical Field

The present invention relates to a resin composition for a resin moldingand to a resin molding.

Related Art

Up to now various kinds of resin compositions have been offered and putto a wide variety of uses.

Resin compositions containing polyolefin in particular have been usede.g. for not only various kinds of components and cabinets of householdelectric appliances and automobiles but also parts such as cabinets ofoffice instruments and electrical-electronic instruments.

SUMMARY

According to an aspect of the invention, a resin composition for resinmoldings includes:

a first resin composition containing a first polyolefin, a polyamide,carbon fibers having an average fiber length of 0.1 mm to 1 mm and acarboxylic anhydride-modified polyolefin as a compatibilizer; and

a second resin composition containing a second polyolefin and organicfibers having an average fiber length of 1 mm to 20 mm,

wherein of the whole quantity of the resin composition for resinmoldings, taking the total contents of the first polyolefin and thesecond polyolefin as 100 parts by mass, a content of the polyamideaccounts for 1 part by mass to 50 parts by mass, a content of the carbonfiber accounts for 1 part by mass to 50 parts by mass, a content of theorganic fibers accounts for 1 part by mass to 20 part by mass, and acontent of the compatibilizer accounts for 1 part by mass to 10 parts bymass.

BRIEF DESCRIPTION OF THE DRAWINGS

Exemplary embodiment(s) of the present invention will be described indetail based on the following figures, wherein:

FIG. 1 is a schematic diagram for illustrating an example of the mainportions of resin moldings relating to embodiments of the invention.

DETAILED DESCRIPTION

Examples of resin compositions and resin moldings according to theinvention are described below.

(Resin Composition for Resin Molding)

A resin composition which relates to an embodiment of the invention andis used for resin moldings (hereafter referred simply to as “a resincomposition” in some cases) includes a first resin compositioncontaining a first polyolefin, a polyamide, carbon fibers having anaverage fiber length of 0.1 mm to 1 mm and a carboxylicanhydride-modified polyolefin as a compatibilizer and a second resincomposition containing a second polyolefin and organic fibers having anaverage fiber length in a range of 1 mm to 20 mm. Additionally, of thetotal quantity by mass of the resin composition for resin moldings,taking the total for the first polyolefin content and the secondpolyolefin content as 100 parts by mass, the polyamide content accountsfor 1 part by mass to 50 parts by mass, the carbon fiber contentaccounts for 1 part by mass to 50 parts by mass, the organic fibercontent accounts for 1 part by mass to 20 parts by mass and thecompatibilizer content account for 1 part by mass to 10 parts by mass.

In other words, the resin composition relating to an embodiment of theinvention includes a first resin composition and a second resincomposition.

The first resin composition contains a first polyolefin, a polyamide,first carbon fibers having an average fiber length of 0.1 mm to 1 mm(hereafter referred simply to as “first carbon fibers” in some cases)and a carboxylic anhydride-modified polyolefin as a compatibilizer.

The second resin composition contains a second polyolefin and secondcarbon fibers having an average fiber length of 6 mm to 20 mm (hereafterreferred simply to as “second carbon fibers” in some cases).

Moreover, of the whole quantity of the resin composition, taking thetotal for a first polyolefin content and a second polyolefin content as100 parts by mass, a polyamide content accounts for 1 part by mass to 50parts by mass, the total for a first carbon fiber content and a secondcarbon fiber content accounts for 1 part by mass to 50 parts by mass anda content of carboxylic anhydride-modified polyolefin as acompatibilizer (hereafter referred simply to as “compatibilizer content”in some cases) accounts for 1 part by mass to 10 parts by mass.

In recent years, resin compositions each containing a polyolefin resinas a base material (matrix) and reinforcing fibers have been used forthe purpose of obtaining resin moldings superior in mechanical strength.

In such resin compositions, when affinity between the reinforcing fibersand the polyolefin is low, spaces develop at the interface between theseingredients, and there may be cases where the spaces cause a reductionin adhesion at the interface.

When a resin composition contains as reinforcing fibers carbon fibers inparticular, though the resin composition is required to ensure highmechanical strengths, notably a high bending elasticity modulus, ascompared with a resin composition containing glass fibers or the like,polar groups contributing adhesion between the reinforcing fibers andthe polyolefin, such as hydroxyl groups and carboxyl groups, present onthe carbon fiber surfaces are small in number as compared with thosepresent on the glass fiber surfaces, and therefore adhesion at carbonfiber-polyolefin interfaces becomes low. As a result, the mechanicalstrengths, notably a bending elasticity modulus, is hard to increase,considering how much the carbon fibers are mixed. When an impact isgiven repeatedly in particular, parting at the carbon fiber-polyolefininterfaces is apt to progress, and hence there develops a tendency toreduce mechanical strengths, notably a bending elasticity modulus, to alarge degree.

As a cause for this tendency, it is presumed that carbon fibers arerigid as compared with glass fibers and other fibrous reinforcing agentsand resist bending distortion when a bending load is imposed thereon,and hence they part from polyolefin surfaces.

With this being the situation, by molding a resin composition containinge.g. 4 ingredients, a polyolefin, carbon fibers, a polyamide and acompatibilizer, the resin molding obtained comes to have excellentmechanical strengths, notably in point of bending elasticity modulus.

In a resin composition containing a polyolefin, carbon fibers, apolyamide and a compatibilizer, when the carbon fibers in the resincomposition include only short fibers (having e.g. an average fiberlength of 1 mm or below), there may be cases where resin moldings madefrom such a resin composition suffer reduction in impact resistance.

For instance, in a resin composition containing carbon fibers, becauseof their rigidity, the carbon fibers are apt to suffer breakage under amechanical load imposed during the process of melt-kneading carbonfibers and a polyolefin. As a result, the carbon fibers in the resincomposition are apt to be reduced in fiber length (e.g. so as to have anaverage fiber length of 1 mm or below).

Thus, as to the composition containing a polyolefin, carbon fibers, apolyamide and a compatibilizer, it has been learned that a resin moldingformed from the resin composition whose carbon fibers are only carbonfibers changed into short fibers by a mechanical load imposed during theprocess of melt-kneading the carbon fibers and the polyolefin, thoughinhibited from reduction in its bending elasticity modulus, has atendency to be susceptible to reduction in impact resistance.

This phenomenon is considered as follows. Because the carbon fibers in aresin molding are changed into those having short lengths, entanglementof carbon fibers is presumed to be limited in the resin molding.Therefore it is presumed that, when an impact force is imposed on theresin molding, the impact force is difficult to diffuse through theinterior of the resin molding to result in breakage of the resinmolding.

In contrast, the resin composition relating to an embodiment of theinvention has the constitution as mentioned above, and thereby resinmoldings obtained therefrom are improved in impact resistance. A reasonfor this improvement remains uncertain, but they are considered asfollows.

The resin composition relating to this embodiment contains carbon fibershaving an average fiber length of 0.1 mm to 1 mm in the first resincomposition and organic fibers having an average fiber length of 1 mm to20 mm in the second resin composition. Organic fibers resist breakageand cutting because of their high elasticity as compared with carbonfibers. As a result, a resin molding formed using this resin compositioncontains organic fibers long in fiber length in addition to carbonfibers having shortened fiber lengths. Specifically, the resin moldingcontains e.g. carbon fibers having an average fiber length in a range of0.1 mm to 1 mm and organic fibers having an average fiber length in arange of 1 mm to 20 mm. And the resin molding is in a state that thepercentage of the number of fibers from 1 mm to 20 mm in fiber length tothe total for the number of carbon fibers and the number of organicfibers is from 1% to 20%.

Under this state, even when impact force is applied on the resinmolding, the impact force is thought to be easy to diffuse into timeinterior of the resin molding. It is therefore presumed that the resinmolding formed using the resin composition having the foregoingconstitution is improved in impact resisting strength.

As mentioned above, the resin composition relating to this embodimentallows, in a resin molding formed therefrom, presence of carbon fibershaving undergone fiber-length shortening and carbon fibers partiallyincluding long fibers, and therefore it is presumed that the resinmolding improved in impact resisting strength is obtained.

Herein, a resin molding obtained using the resin composition relating toan embodiment of the invention is also inhibited from receivingreduction in bending elasticity modulus. Although an action bringingabout such an effect remains unclear, it is thought as follows.

On the occasion of producing a resin molding from the resin compositionwhich relates to an embodiment of the invention and includes the firstresin composition and the second resin composition, the resincomposition is subjected to hot-melt mixing, and thereby the polyolefinas a matrix and the compatibilizer are molten together, and besides thepolyamide becomes compatible with the compatiblizer through a portion ofthe interior of compatibilizer molecules and amide or imide bondspresent in polyamide molecules, resulting in dispersion into the resincomposition.

By the way, the term polyamide as used in this specification is intendedto include not only resins having amide bonds in their individual mainchains but also resins having both amide bonds and imide bonds in theirindividual main chains (referred to as the so-called polyamide imide).

In the state described above, when polyamide molecules come into contactwith carbon fibers (including the first carbon fibers and the secondcarbon fibers), amide bonds or imide bonds present in large numbersalong the molecular chains of polyamide and polar groups present insmall numbers on carbon fiber surfaces are physically coupled togetherat multiple sites by dint of affinity (gravitation and hydrogenbonding). In addition, because not only compatibility of polyolefin withcarbon fiber but also affinity of polyolefin for carbon fiber isgenerally low, repulsive force is created between polyolefin andpolyamide as well as between polyolefin and carbon fiber, and therebyfrequency of contact between polyamide and carbon fiber is increased,resulting in formation of domains of carbon fiber-polyamide compositesin the polyolefin matrix. Consequently, the amount and area of polyamidebonded to carbon fibers are increased. Thus a covering layer ofpolyamide is formed around the periphery of carbon fiber (see FIG. 1).By the way, PP, CF, and CL in FIG. 1 stand for polyolefin, carbon fiberand covering layer, respectively.

Further, the polyamide forming a covering layer chemically reacts withsome of reactive groups in compatibilizer molecules, and electrostaticinteractions occur between polar groups in these ingredients, andthereby the polyamide comes to have compatibility with thecompatibilizer, and besides the compatibilizer is also compatible withpolyolefin. Thus an equilibrium state is created between gravitationaland repulsive forces to result in formation of a polyamide coveringlayer in a thin and uniform state. Because affinity of carboxyl groupspresent on the carbon fiber surfaces for amide bonds or imide bondspresent in polyamide molecules is especially high, it is presumed that acovering layer of polyamide is more likely to be formed around theperipheries of carbon fibers, and the covering layer formed is thin andsuperior in uniformity.

In addition, the covering layer preferably covers all over the carbonfiber surface, but an uncovered portion may be present on the carbonfiber surface.

As mentioned above, the resin composition relating to an embodiment ofthe invention allows improvement in adhesion of the carbonfiber-polyolefin interface. Consequently, it is considered that resinmoldings obtained from the resin composition relating to an embodimentof the invention is superior in mechanical strengths, notably in bendingelasticity modulus.

As to the resin composition relating to an embodiment of the inventionand including the first resin composition and the second resincomposition and resin moldings obtained from such a resin composition, acovering layer of polyamide is formed around the peripheries of carbonfibers through the hot-melt kneading during the preparation for thefirst resin composition (in the form of e.g. pellets) and injectionmolding of the resin composition, and the covering layer formedpreferably has a structure from 5 nm to 700 nm in thickness.

In the resin composition relating to an embodiment of the invention, thecovering layer of polyamide is from 5 nm to 700 nm in thickness, andfrom the viewpoint of further improving the bending elasticity modulus,the thickness thereof is preferably from 10 nm to 650 nm. The coveringlayer thickness of 5 nm or above (notably 10 nm or above) allowsimprovement in bending elasticity modulus, while the covering layerthickness of 700 nm or below makes it possible to inhibit the interfacebetween carbon fiber and polyolefin through the medium of polyamide frombecoming fragile, thereby controlling reduction in bending elasticitymodulus.

The thickness of the covering layer is a value determined by thefollowing method. A subject of measurement is ruptured in liquidnitrogen, and a cross section thereof is observed an electron microscope(VE-9800, made by KEYENCE CORPORATION). On the cross section, thicknessmeasurements are made at 100 points of covering layers covering aroundthe peripheries of carbon fibers, and the average of these measurementvalues is calculated.

By the way, checking of the covering layers is carried out by the crosssection observation mentioned above.

Additionally, the first resin composition included in the resincomposition relating to an embodiment of the invention and a resinmolding molded from the resin composition relating to an embodiment ofthe invention and including the first resin composition and the secondresin composition have structure that the compatibilizer performspartial compatibilization between the covering layer and the polyolefin.

To be specific, it is appropriate that there be an intervening layer ofcompatibilizer e.g. between the polyamide covering layer and thepolyolefin as a matrix (see FIG. 1). In other words, it is appropriatethat a layer of the compatibilizer be formed on the surface of thecovering layer and the covering layer be adjacent to the polyolefinthrough the layer of the compatibilizer. The layer of the compatibilizeris formed in a smaller thickness than the covering layer, and theadhesion (bonding) of the covering layer to the polyolefin is enhancedby the medium of the compatibilizer layer, and thereby it becomes easyto obtain a resin molding superior in mechanical strengths, notably inbending elasticity modulus. By the way, PP, CF, CL and CA in FIG. 1stand for polyolefin, carbon fiber, covering layer and compatibilizer,respectively.

It is especially appropriate that the compatibilizer layer be presentbetween the covering layer and the polyolefin in a state of bonding tothe coveting layer (through hydrogen bonds and covalent bonds formed byreaction between functional groups of the compatibilizer and thepolyamide) and being compatible with the polyolefin. Such a constitutionis easy to realize by adopting a compatibilizer which has e.g. the samestructure as the polyolefin matrix or a structure allowing compatibilitywith the polyolefin, and besides which contains in a portion of itsmolecule such a moiety as to react with the above-cited functionalgroups of the polyamide.

More specifically, in the case of adopting e.g. a polyolefin, apolyamide and a maleic anhydride-modified polyolefin as acompatibilizer, it is appropriate that a layer of the maleicanhydride-modified polyolefin (a layer of the compatibilizer) be presentin a state that the carboxyl groups formed by ring-opening, of maleicanhydride moieties react with amine residues of the polyamide layer(covering layer) to bond these layers together and compatibilize suchpolyolefin moieties and the polyolefin.

Now, a method for checking the presence of a compatibilizer layerbetween the covering layer and the polyolefin is as follows.

An infrared microspectroscopic analyzer (IRT-5200, made by JASCOCorporation) is used as an analysis device. For example, a sliced pieceis cut from a resin molding which includes polypropylene (PP) as apolyolefin, PA66 as a polyamide and maleic anhydride-modified polyolefin(MA-PP) as a modified polyolefin, and a cross section thereof isobserved. IR mapping of covering layer portions around the crosssections of carbon fibers is carried out, thereby checking on coveringlayer-maleic anhydride of compatibilizer layer origin (1,820 cm⁻¹ to1,750 cm⁻). By doing so, the presence of a compatibilizer layer betweenthe covering layer and the polyolefin can be ascertained. Morespecifically, when reaction occurs between MA-PP and PA66, cyclicmaleated portion of MA-PP undergoes ring opening, and thereby chemicalbonding of the amine residues of PA66 takes place to reduce the cyclicmaleated portion. Thus the presence of a compatibilizer layer (bondinglayer) between the covering layer and the polyolefin can be ascertained.

(First Resin Composition and Second Resin Composition)

The resin composition relating to an embodiment of the invention, asmentioned above, has the first resin composition containing a firstpolyolefin, a polyamide, first carbon fibers and a compatibilizer, andbesides it has the second resin composition containing a secondpolyolefin and second carbon fibers.

Additionally, it is appropriate that each of the first resin compositionand the second resin composition be a non-crosslinked resin composition.

Herein, the second resin composition may consist of two ingredients, asecond polyolefin and second carbon fibers, or it may contain, inaddition to these two ingredients, at least either a second polyamide ora carboxylic anhydride-modified polyolefin as a second compatibilizer.

In the resin composition relating to an embodiment of the invention, theratio (by mass) between the first resin composition and the second resincomposition has no particular limits. The ratio between these two resincompositions may be determined so that, taking the total content of thefirst polyolefin and the second polyolefin as 100 parts by mass,referred to the whole quantity of the resin composition, the polyamidecontent falls within a range of 1 part by mass to 50 parts by mass, thetotal content of the first carbon fibers and the second carbon fibersfalls within a range of 1 part by mass to 50 parts by mass and thecompatibilizer content falls within a range of 1 part by mass to 10parts by mass.

As to the ratio between the first resin composition content and thesecond resin composition content, depending on the ingredients of thefirst resin composition and those of the second resin compositions, whenthe first resin composition content of the whole resin composition issymbolized by W1 and the second resin composition content of the wholeresin composition is symbolized by W2, the W1/W2 ratio by mass is e.g. W1/W2=1/99 to 99/1 (preferably from 10/90 to 90/10).

In point of improvement in impact resistance of a resin molding to beformed, it is appropriate that the proportion of each of ingredients, afirst polyolefin, a polyamide, first carbon fibers and a compatibilizer,in the first resin composition be within a range as specified below.

It is appropriate that the polyolefin content of the first resincomposition account for e.g. from 5 mass % to 95 mass % (preferably from10 mass % to 95 mass %, more preferably from 20 mass % to 95 mass %) ofthe total mass of the first resin composition.

It is appropriate that the polyamide content of the first resincomposition be from 0.1 parts by mass to 100 parts by mass (preferablyfrom 0.5 parts by mass to 90 parts by mass, more preferably from 1 partby mass to 80 pars by mass) with respect to 100 parts by mass of thepolyolefin.

It is appropriate that the first carbon fiber content of the first resincomposition be from 0.1 parts by mass to 200 parts by mass (preferablyfrom 1 part by mass to 180 parts by mass, more preferably from 5 partsby mass to 150 pars by mass) with respect to 100 parts by mass of thepolyolefin.

It is appropriate that the compatibilizer content of the first resincomposition be from 0.1 parts by mass to 50 parts by mass (preferablyfrom 0.1 parts by mass to 40 parts by mass, more preferably from 0.1parts by mass to 30 pars by mass) with respect to 100 parts by mass ofthe polyolefin.

Further, it is appropriate in point of improvement in impact resistanceof a resin molding to be formed that the proportion of each ofingredients, a second polyolefin and second carbon fibers, in the secondresin composition be within a range as specified below.

It is appropriate that the polyolefin content of the second resincomposition account for e.g. from 40 mass % to 90 mass % (preferablyfrom 50 mass % to 80 mass %) of the total mass of the second resincomposition.

It is appropriate that the second carbon fiber content of the secondresin composition be from 11 parts by mass to 150 parts by mass(preferably from 25 parts by mass to 100 parts by mass) with respect to100 parts by mass of the polyolefin.

In point of improvement in impact resistance, it is appropriate that theratio (by mass) between the carbon fibers in the first resin compositionand the organic fibers in the second resin composition fall within therange as specified below.

When the carbon fiber content and the organic fiber content, referred tothe whole quantity of the resin composition for a resin molding, aresymbolized by CF1 and OF2, respectively, it is appropriate that theratio by mass between CF1 and OF2 (CF1/OF2 ratio) be from at leastCF1/OF2=60/40 to at most CF1/OF2=99/1 (preferably from at least 70/30 toat most 95/5). Additionally, when the organic fiber content becomeshigher, the bending elasticity modulus is more likely to deteriorate.

(Manufacturing Method of Resin Composition)

The first resin composition is manufactured by a method in which a firstpolyolefin, a polyamide, carbon fibers cut down to an intended lengthand a compatibilizer are subjected to melt kneading.

Herein, publicly-known systems can be used as melt kneading instruments,with examples including a twin-screw extruder, a Henschel mixer, aBanbury mixer, a single-screw extruder, a multi-screw extruder and aco-kneader.

The temperature during the melt kneading (cylinder temperature) may bedetermined in response to the melting temperatures of resinousingredients and the like included in the resin composition.

It is preferred that the first resin composition in particular beobtained by a manufacturing method including the process of subjecting apolyolefin, a polyamide, carbon fibers cut down to an intended lengthand a compatibilizer to melt kneading. When a set of polyolefin,polyamide and carbon fibers cut down to the intended length andcompatibilizer is melt-kneaded as a single unit, a covering layer of thepolyamide in a thin and nearly uniform state tends to be formed aroundthe periphery of each individual carbon fiber, thereby allowingimprovements in mechanical strengths, notably in bending elasticitymodulus.

As an example of a method for manufacturing the second resincomposition, mention may be made of a method in which a secondpolyolefin and long-length organic fibers cut down to an intended lengthare subjected to melt kneading. As another example, mention may be madeof a method in which, while the organic fibers in continuous fiber form(known as roving) are subjected to opening, the surfaces thereof areimpregnated and coated with a molten polyolefin resin, and the thusprocessed carbon fibers are pulled out (a pultrusion process). From theviewpoint of inhibiting breakage of the organic fibers, it is preferredthat the second resin composition in particular be manufactured throughthe use of such a pultrusion process.

As an example of a pultrusion process, mention ay be made of apublicly-known method. To be more specific, in such a method, carbonfibers in continuous fiber form are impregnated and coated with a moltenpolyolefin by means of e.g. a cross-head die. After solidification bycooling, the resulting carbon fibers are cut down to an intended length,and thereby made into the second resin composition.

By using any of the foregoing methods is obtained a resin compositionwhich relates to an embodiment of the invention and includes the firstresin composition and the second resin composition. By the way, theresin composition relating to an embodiment of the invention may be acomposition obtained by mixing the first resin composition and thesecond resin composition, or it may also be a composition obtained bymixing the first resin composition and the second resin composition, andthen melting both the first resin composition and the second resincomposition.

(Constitution of Resin Composition)

In the next place, proportions of individual ingredient contents in thewhole quantity of the resin composition are described.

The resin composition relating to this embodiment of the invention has,as mentioned above, ingredient contents in their respective proportionsspecified below in the whole quantity of the resin composition includingthe first resin composition and the second resin composition.

With respect to 100 parts by mass of total content of the firstpolyolefin and the second polyolefin, the polyamide content is from 1part by mass to 50 parts by mass, the carbon fiber content is from 1part by mass to 50 parts by mass, the organic fibers is from 1 part bymass to 20 parts by mass and the compatibilizer content is from 1 partto 10 parts by mass.

The percentage of a polyolefin content (total for a first polyolefincontent and a second polyolefin content) to the whole mass of resincomposition may be determined in response to uses of a resulting resinmolding. For example, the polyolefin content accounts for preferably 5mass % to 95 mass %, more preferably 10 mass % to 95 mass %, still morepreferably 20 mass % to 95 mass %, of the total mass of resincomposition.

The carbon fiber content is from 1 part by mass to 50 parts by mass,preferably from 10 parts by mass to 50 parts by mass, more preferablyfrom 20 parts by mass to 40 parts by mass, referred to 100 parts by massof polyolefin.

By containing carbon fibers in a proportion of at least 1 part by mass,referred to 100 parts by mass of polyolefin, the resin composition aimsreinforcement, and by adjusting the carbon fiber content to 50 parts bymass or below, referred to 100 parts by mass of polyolefin, goodmoldability is achieved at the time of producing a resin molding.

Hereafter, a content (by mass) with respect to 100 parts by mass ofpolyolefin is abbreviated as phr (per hundred resin) in some cases.

Using this abbreviation, the above phrase is expressed as “carbon fibercontent is from 1 phr to 50 phr”.

The organic fiber content is from 1 part by mass to 20 parts by mass,preferably from 2 parts by mass to 15 parts by mass, more preferablyfrom 5 parts by mass to 15 parts by mass, referred to 100 parts by massof polyolefin.

By containing organic fibers in a proportion of at least 1 part by mass,referred to 100 parts by mass of polyolefin, the resin composition aimsreinforcement and can achieve improvement in impact resistance, and byadjusting the organic fiber content to 20 parts by mass or below,referred to 100 parts by mass of polyolefin, good moldability isachieved at the time of producing a resin molding.

By the way, in the case of using a fibrous reinforcing agent other thancarbon fibers and organic fibers, it is appropriate that the total for acarbon fiber content and an organic fiber content account for at least90% by mass of the total for the carbon fiber content, the organic fibercontent and the fibrous reinforcing agent content.

The polyamide content is from 1 part by mass to 50 parts by mass,refereed to 100 parts by mass of polyolefin. From the viewpoint offurther enhancing impact resistance, the polyamide content is preferablyfrom 2 parts by mass to 40 part by mass, more preferably from 5 parts bymass to 30 parts by mass.

By adjusting the polyamide content to fall within the above range, theaffinity for the carbon fibers is increased, and enhancement of impactresistance is aimed at.

In the special case of containing a polyamide in a large amount rangingfrom larger than 1 parts by mass to no larger than 50 parts by mass withrespect to 100 parts by mass of polyolefin, the compatibilizer contentrelative to the polyamide content becomes low, and thereby it becomesdifficult for the polyamide to di se into the polyolefin matrix and atendency for the polyamide to localize around the peripheries of carbonfibers is intensified. Thus it is thought that a covering layer ofpolyamide is formed in a somewhat-thickened and nearly-uniform state allover the peripheries of the carbon fibers having short fiber lengths.Therefore adhesion at the interfaces between polyolefin and carbonfibers is enhanced, and it becomes easy to obtain a resin moldingsuperior in mechanical strengths, notably in impact resistance.

From the viewpoint of allowing an affinity of polyamide for carbonfibers to manifest itself effectively and increasing flowability of theresin composition, it is preferred that the polyamide content beproportioned to the foregoing carbon fiber content.

The compatibilizer content is from 1 part by mass to 10 parts by mass,preferably from 1 part by mass to 8 parts by mass, more preferably from1 part by mass to 5 parts by mass, with respect to 100 parts by mass ofpolyolefin.

By adjusting the compatibilizer content to fall within the above range,the affinity between polyolefin and polyamide is enhanced, and therebyimprovement in impact resistance is aimed at.

From the viewpoint of enhancing the affinity between polyolefin andpolyamide, it is preferred that the compatibilizer content beproportioned to the polyamide content (and be proportioned indirectly tothe carbon filter content).

Each of ingredients in the resin composition relating to an embodimentof the invention is described below in detail.

—Polyolefin—

The resin composition which relates to an embodiment of the inventionand is used for resin moldings contains a first polyolefin in the firstresin composition and a second polyolefin in the second resincomposition.

The first polyolefin and the second polyolefin may be the same as ordifferent from each other, but they are preferably the same. Inaddition, as each of polyolefin for the first polyolefin and that forthe second polyolefin, only one kind may be used or two or more kinds ofpolyolefin may be used in combination.

Hereafter, as to particulars common to the first polyolefin and thesecond polyolefin, explanation is made by simply using the termpolyolefin so long as there is no need to make a distinction betweenthem.

Polyolefin is a matrix of the resin composition, and refers to theresinous ingredient to be reinforced by carbon fibers (which is alsoreferred to as a matrix resin).

Polyolefin is a resin containing repeating units of olefin origin, andthe resin may contain repeating units derived from a monomer other thanolefins so long as the other repeating units constitute at most 30 mass% of the whole resin.

Polyolefin is produced by addition polymerization of an olefin (and, ifnecessary, a monomer other than olefins).

In addition, each of the olefin and the monomer other than olefins foruse in production of polyolefin may be only one kind or a combination oftwo or more kinds.

By the way, the polyolefin may be either a homopolymer or a copolymer.Additionally, the polyolefin may have the form of either a straightchain or a branched chain.

Examples of such olefins include straight-chain or branched-chainaliphatic olefins and alicyclic olefins.

Examples of aliphatic olefins include α-olefins, such as ethylene,propylene, 1-butene, 1-hexene, 4-methyl-1-pentene, 1-octene, 1-decene,1-hexadecene and 1-octadecene.

On the other hands, examples of alicyclic olefins include cyclopentene,cyclobutene, cycloheptene, norbornene, 5-methyl-2-norbornene,tetracyclododecene and vinylcyclohexene.

Of these olefins, in point of cost, α-olefins are preferable to theothers, ethylene and propylene are far preferred, and propylene isespecially preferred.

Also, well-known addition-polymerizable compounds are selected as amonomer other than olefins.

Examples of the addition-polymerizable compound include styrenecompounds, such as styrene, methylstyrene, α-methylstyrene,β-methylstyrene, t-butylstyrene, chlorostyrene, chloromethylstyrene,methoxystyrene and styrene sulfonic acid or salts thereof; (meth)acrylicesters, such as alkyl (meth)acrylates, benzyl (meth)acrylate anddimethylaminoethyl (meth)acrylate; halovinyl compounds, such as vinylchloride; vinyl esters such as vinyl acetate and vinyl propionate; vinylethers, such as vinyl methyl ether; halogenated vinylidene compounds,such as vinylidene chloride; and N-vinyl compounds, such asN-vinylpyrrolidone.

Examples of a suitable polyolefin include polypropylene (PP),polyethylene (PE) and ethylene-vinyl acetate copolymer resin (EVA). Itis appropriate that the polyolefin be at least one kind selected fromthe group consisting of polypropylene (PP), polyethylene (PE) andethylene-vinyl acetate copolymer resin (EVA).

Among the olefin polymers recited above, resins each containing onlyrepeating units of olefin origin are preferred over the others, andpolypropylene is especially preferred in point of cost.

The molecular weight of polyolefin is not particularly limited, and itmay be determined in response to the kind of resin used, moldingconditions, uses of resulting resin moldings and so on. For example, theweight-average molecular weight (Mw) of polyolefin is preferably in arange of 10,000 to 300,000, more preferably in a range of 10,000 to200,000.

In addition, the glass transition temperature (Tg) or meltingtemperature (Tm) of polyolefin is not particularly limited as is thecase with the molecular weight, and it may be determined in response tothe kind of resin used, molding conditions, uses of resulting resinmoldings and so on. For example, the melting temperature (Tm) ofpolyolefin is preferably in a range of 100° C. to 300° C., morepreferably in a range of 150° C. to 250° C., still more preferably in arange of150° to 200° C., most preferably in a range of 160° C. to 190°C.

By the way, the weight-average molecular weight (Mw) and meltingtemperature (Tm) of polyolefin are values determined as follows.

Specifically, the weight-average molecular weight (Mw) of polyolefin isdetermined by using gel permeation chromatography (GPC) under thefollowing conditions. A high-temperature GPC system HLC-8321GPC/HT isused as GPC apparatus and o-dichlorobenzene is used as an eluent. Apolyolefin is once molten in o-dichlorobenzene and filtered at a hightemperature (a temperature in a range of 140° C. to 150° C.), and thefiltrate thus obtained is adopted as a measurement sample. As to themeasurement conditions, the sample concentration is 0.5%, the flow rateis 0.6 ml/min, the injected sample volume is 10 μl, and the measurementis made with an RI detector. In addition, the calibration curve isprepared using 10 polystyrene standard samples produced by TOSOHCORPORATION, TSK standard A-500, F-1, F-10, F-80, F-380, A-2500, F-4,F-40, F-128 and F-700.

On the other hand, the melting temperature (Tm) of polyolefin isdetermined from the DSC curve obtained by differential scanningcalorimetry (DSC) as “melting peak temperature” described in JIS K7121-1987, directions for determination of melting temperature in“methods for measuring transition temperature of plastic”.

—Carbon Fiber—

The resin composition relating to an embodiment of the inventioncontains carbon fibers having an average fiber length of 0.1 mm to 1 mmin the first resin composition.

The average fiber length of carbon fibers is preferably from 0.1 mm to0.8 mm, more preferably from 0.2 mm to 0.8 mm.

A method for measuring fiber lengths of the carbon fibers will bedescribed later.

As the carbon fibers used when the first resin composition is prepared,carbon fibers having an average fiber length of e.g. 0.1 mm to 5.0 mmare suitable. For example, carbon fibers having an average fiber lengthof 0.1 mm to 1 mm may be used, or those having an average fiber lengthsof 1 mm to 5 mm may be used. Even when carbon fibers have an averagefiber length of 1 mm to 5 mm, they may be used if only the average fiberlength is adjusted to fall within the range of 0.1 mm to 1 mm during themelt-kneading process.

When the average fiber length of carbon fibers in the first resincomposition is in the above range, reduction in flowability at the timeof melting the resin composition is inhibited. Further, reduction inbending elasticity modulus of a resulting resin molding is alsoinhibited.

As the carbon fibers, publicly-known carbon fibers are used, and any ofPAN-based carbon fibers and pitch-based carbon fibers may be used.

The carbon fibers may be those having undergone publicly-known surfacetreatment.

Examples of surface treatment for carbon fibers include oxidizingtreatment and sizing treatment.

As the carbon fibers, commercially available products may be used.

Examples of a commercially available PAN-based carbon fiber productinclude TORAYCA®, produced by Toray Industries, Inc., Tenax produced byToho Tenax, and Pyrofil®, produced by Mitsubishi Chemical Corporation.In addition thereto, commercially available PAN-based carbon fiberproducts include products from Hexcel Corporation, those from CytecIndustries, Inc., those from DowAksa, those from Formosa PlasticsCorporation, those from SGL and so on.

Examples of a commercially available pitch-based carbon fiber productinclude DIALEAD® produced by Mitsubishi Chemical Corporation, GRANOCproduced by Nippon Graphite Fiber Co., Ltd., and KURECA produced byKUREHA CORPORATION. In addition thereto, commercially availablepitch-based carbon fiber products include products from Osaka GasChemicals Co., Ltd., those from Cytec Industries, Inc. and so on.

By the way, only one kind of carbon fibers may be used, or two or moredifferent kinds of carbon fibers may be used in combination.

The carbon fibers have no particular limits on their fiber diameter andso on, and the fiber diameter may be chosen according to the uses of aresulting resin molding. The average fiber diameter of carbon fibers maybe e.g. from 5.0 μm to 10.0 μm (preferably from 6.0 μm to 8.0 μm).

Herein, the average fiber diameter of carbon fibers is determined in thefollowing manner. A cross section orthogonal to the length direction ofeach individual carbon fiber is observed under an SEM (a scanningelectron microscope) set at a magnification of 1,000, and the diameterof each individual carbon fiber is measured. This measurement is made on100 carbon fibers, and the average of measured values is calculated anddefined as the average diameter of carbon fibers.

—Organic Fibers—

The resin composition relating to this embodiment contains organicfibers having an average fiber length of 1 mm to 20 mm in the secondresin composition. The average fiber length of organic fibers ispreferably from 2 mm to 18 mm, more preferably from 6 mm to 15 mm.

The organic fibers included in the second resin composition has noparticular restrictions so long as their average fiber length is in arange of 1 mm to 20 mm. In point of improvement in impact resistance ofresulting resin moldings, it is appropriate to use organic fibers of thetype which is produced by Roving method and made up of great many fibersin a converged state.

The organic fibers has no particular restriction, but from the viewpointof incorporating them into the second resin composition and resinmoldings, it is appropriate for the organic fibers to resist meltingwhen they are heated for production of the second resin composition andresin moldings. In this respect, it is appropriate that the meltingpoint, softening point or thermal decomposition temperature of organicfibers be higher than the melting point of polyolefin. For example, itis appropriate that the melting point, softening point and thermaldecomposition temperature of organic fibers be at least 5° C. higherthan the melting point of polyolefin. Such a temperature of organicfibers has no particular upper limit, but the upper limit thereof may bee.g. 200° C. or lower.

Additionally, the melting point, softening point or thermaldecomposition temperature of organic fibers is measured as follows.

The melting point of organic fibers can be determined by the same methodas used for melting-point measurement made on polyolefin. Specifically,the melting point of organic fibers is determined from the DSC curveobtained by differential scanning calorimetry (DSC) as “melting peaktemperature” described in JIS K 7121-1987, directions for determinationof melting temperature in “methods for measuring transition temperatureof plastic”.

The softening point of organic fibers is determined in conformance with.JIS K 7206-2016, “methods for determining Vicat softening temperature(VST) of plastics-thermoplastic plastic”.

The thermal decomposition temperature of organic fibers is determinedfrom a TG curve obtained by thermogravimetric measurement (TG)conforming to JIS K 7121-1987, “methods for thermogravimetricmeasurement of plastic”, as the temperature at which weight reduction ofa sample begins.

Examples of organic fibers include fibers formed from resins termed“engineering plastics”.

To be more specific, examples of organic fibers include ultrahighmolecular-weight polyethylene fibers; polycarbonate fibers, polyarylatefibers, polyoxymethylene fibers; polyester fibers, such as polybutyleneterephthalate fibers, polybutylene naphthalate fibers andliquid-crystalline aromatic polyethylene terephthalate fibers;polybenzazole fibers, such as polyparaphenylene benzobisoxazole (PBO)fibers and polyparaphenylenebenzobisthiazole fibers; polyphenylenesulfide fibers; modified polyphenylene ether fibers; polyimide fiberssuch as nylon fibers; and aramide fibers such as poly-p-phenyleneterephthalamide fibers and poly-m-phenylene isophthalamide fibers. Also,in addition to the above organic fibers, the organic fibers such asvinylon fibers and cellulose fibers are exemplified.

These organic fibers may be used alone, or two or more kinds thereof maybe used in combination.

Of those organic fibers, at least one kind of organic fibers selectedfrom the group consisting of aramide fibers, vinylon fibers andcellulose fiber are suitable, at least one kind selected from aramidefibers or vinylon fibers is preferred, and aramide fibers are muchpreferred.

Aramide is also described as all-aromatic polyamide, and refers tofibrous polyamide constituted of structural units containing aromaticrings in its molecular skeleton. The aramide fibers are generallyobtained using as a raw material an aramide synthesized bycopolymerization of diamine and dicarboxylic acid.

As aramide fibers, publicaly known aramide fiber are used, and morespecifically, either of para-type aramide fibers (e.g. poly-p-phenyleneterephthalamide fibers) and meta-type aramide fibers (e.g.poly-m-phenyleneisophthalamide fibers) can be used.

The aramide fibers may be those having undergone publicly-known surfacetreatment. Examples of surface treatment for aramide fibers includeoxidizing treatment and sizing treatment.

The aramide fibers have no particular restrictions as to their fiberdiameter, and the fiber diameter may be chosen in response to the usesof a resulting resin molding. The average fiber diameter of aramidefibers may be e.g. from 5.0 μm to 100 μm (preferably from 10 μm to 20μm).

The average fiber diameter of aramide fibers is determined as follows. Across section orthogonal to the length direction of each individualaramide fiber is observed under an SEM (a scanning electron microscope)set at a magnification of 1,000, and the diameter of each individualaramide fiber is measured. This measurement is made on 100 aramidefibers, and the average of measured values is calculated and defined asthe average diameter of aramide fibers.

Vinylon fibers are e.g. fibers obtained using polyvinyl alcohol as a rawmaterial.

As the vinylon fibers, publicly-known vinylon fibers are used. Thevinylon fibers may be those having undergone surface treatment.

As the cellulose fibers, publicly-known cellulose fibers are used, withexamples including fibers obtained using as a raw material naturalcellulose fibers such as cotton or jute.

Fiber diameters of vinylon fibers and cellulose fibers have noparticular limits, and they may be chosen in response to e.g. uses ofresulting resin moldings.

Now, there are provided explanation of a method for measuring the fiberlengths of carbon fibers and organic fibers included in a resincomposition and the fiber lengths of carbon fibers and organic fibersincluded in a resin molding as described later.

To begin with, a subject for measurement, namely a resin composition ora resin molding, is put in an aluminum crucible, and fired at 500° C.for 2 hours by means of a Muffle furnace. After the firing, the carbonfibers remaining in the crucible are collected, and dispersed into a0.1% water solution of surfactant. Photographs of the carbon fibers aretaken using a digital microscope (VHX-100, made by KEYENCE CORPORATION)under a measurement magnification of 10. The fiber lengths of carbonfibers are measured using image analysis software (WINROOF2015, producedby MITANI CORPORATION). And this fiber-length measurement is made on 200carbon fibers, and the average value of fiber lengths thus measured isdefined as an average fiber length of carbon fibers. By the way, thefiber length of carbon fibers is a number-average fiber length.

By the way, there may be cases where, depending on organic fibersincluded in the resin composition or the resin molding as a subject formeasurement, melting or disappearance of the organic fibers occurs whenthe subject for measurement is fired at 500° C. for 2 hours, and therebyaverage fiber-length measurement becomes difficult. In such cases,average fiber-length measurement on organic fibers can be made asfollows.

A resin composition or a resin molding is dissolved in an organic polarsolvent such as N-methyl-2-pyrrolidone and heated under reflux for 72hours, and thereby the polyamide as a resinous ingredient in the resincomposition or the resin molding is brought into at least either adissolved or swollen state. Organic fibers are removed from organicfiber-bearing residue, and organic fiber lengths are measured accordingto the measurement method mentioned above.

—Polyamide—

Polyamide is a resin having amide bonds. The polyamide include a resinhaving amide bonds in one and the same main chain thereof and a resinhaving imide bonds as well as amide bonds in one and the same main chainthereof.

Such polyamide is illustrated below in detail.

The polyamide is preferably a resin low in compatibility withpolyolefin, and more specifically, a resin different in solubilityparameter (SP value) from polyolefin.

Herein, the SP value difference between polyolefin and polyamide ispreferably at least 3, more preferably from 3 to 6, from the viewpointsof compatibility between these polymers and repulsive force betweenboth.

The SP value mentioned herein is a value estimated by the Fedors method.More specifically, the solubility parameter (SP value) conforms e.g. tothe description in Polymer. Eng. Sci., vol. 14, p.147 (1974), and it isdetermined by the following expression.

Expression: SP value=√(Ev/v)=√(ΣΔei/ΣΔvi)

(In the expression, Ev is evaporation energy (cal/mol), v is molarvolume (cm³/mol), Δei is evaporation energy of each individual atom oratomic group and Δvi is molar volume of each individual atom or atomicgroup).

By the way, (cal/cm³)^(1/2) is adopted as a unit of solubility parameter(SP value), but herein the unit is omitted according to establishedpractice and dimensionless notation is used.

In addition, the polyamide has amide bonds in its molecule.

By virtue of presence of amide bonds in polyamide, an affinity developsbetween the polyamide and polar groups present on the surface of carbonfiber.

As one among concrete kinds of the polyamide, there is a thermoplasticresin containing amide bonds in its main chain, and examples thereofinclude polyamide (PA), polyamide imide (PAI) and polyamino acid.

The polyamide has no particular restrictions, but from the viewpoints offurther enhancement of impact resistance and excellent adhesion tocarbon fibers, polyamide (PA) is preferred.

Examples of the polyamide include polyamide produced bycopolycondensation of dicarboxylic acid and diamine and polyamideproduced by condensation of lactam. More specifically, the polyamide ise.g. a polyamide having at least either structural units formed bypolycondensation of dicarboxylic acid and diamine or structural unitsformed by ring-opening of lactam.

When polyamide having aromatic ring-containing structural units exceptaramide structural units and aromatic ring-free structural units isutilized as the polyamide, the polyamide can have good affinities forboth of carbon fiber and polyolefin. Now, polyamide having only aromaticring-containing structural units tends to be high in affinity for carbonfiber and low in affinity for polyolefin as compared with polyamidehaving only aromatic ring-free structural units. Polyamide having onlyaromatic ring-free structural units tends to be low in affinity forcarbon fiber and high in affinity for polyolefin as compared withpolyamide containing only aromatic ring-containing structural units. Onthis account, utilization of polyamide having both of these structuralunits ensures good affinities for both carbon fiber and polyolefin, anda covering layer formed of such a polyamide allows further enhancementof adhesion at the interface between carbon fiber and polyolefin.Therefore resin moldings superior in mechanical strengths, notably inimpact resistance, become easy to obtain.

In addition, utilization of polyamide having both ring-containingstructural units and aromatic ring-free structural unit conduces to notonly reduction in melt viscosity but also improvement in moldability(e.g. injection moldability). Accordingly, resin moldings high inoutward appearance quality become easy to obtain.

On the other hand, utilization of polyamide having only aramidestructural units brings about thermal degradation of polyolefin at hightemperatures allowing fusion of the polyamide. Moreover, satisfactoryfusion of the polyamide does not occur at temperatures causing thermaldegradation of polyolefin, resulting in deterioration of moldability(e.g. injection moldability) and reductions in outward appearancequality and mechanical performance of resin moldings to be produced.

By the way, the term aromatic ring used herein is intended to include 5-or more-membered monocyclic aromatic rings (e.g. cyclopentadiene,benzene) and fused rings (e.g. naphthalene) formed by fusing togethertwo or more 5- or more-membered monocyclic aromatic rings. The aromaticrings include heterocyclic rings (e.g. pyridine) also.

In addition, the aramide structural unit refers to the structural unitformed by polycondensation reaction between an aromatic ring-containingdicarboxylic acid and an aromatic ring-containing diamine.

The aromatic ring-containing structural unit except the aramidestructural unit includes e.g. at least either of the followingstructural units (1) and (2).

-   Structural unit (1): —(—NH—Ar¹—NH—CO—R¹—CO—)— (where Ar¹ represents    a divalent organic group which contains an aromatic ring, and R¹    represents a divalent organic group which is free of an aromatic    ring)-   Structural unit (2): —(—NH—R²—NH—CO—Ar²—CO—)— (where Ar² represent a    divalent organic group which contains an aromatic ring, and R²    represents a divalent organic group which is free of an aromatic    ring)

On the other hand, the aromatic ring-free structural unit includes e.g.at least either of the following structural units (3) and (4).

-   Structural unit (3): —(—NH—R³¹—NH—CO—R³²—CO—)— (where R³¹ represent    a divalent organic group which is free of an aromatic ring, and R³²    represents a divalent organic group which is free of an aromatic    ring)-   Structural unit (4): —(—NH—R⁴—CO—)— (where R⁴ represents a divalent    organic group which is free of an aromatic ring)

By the way, the divalent organic groups represented by individualsymbols in structural formulae (1) to (3) are organic groups derivedfrom divalent organic groups present in dicarboxylic acids, diamines orlactams. To be more specific, the divalent organic group which containsan aromatic ring and is represented e.g. by Ar¹ in the structural unit(1) refers to the residue formed by removing two amino groups fromdiamine, and the divalent organic group which is free of an aromaticgroup and represented e.g. by R¹ in the structural unit (1) refers tothe residue formed by removing two carboxyl groups from a dicarboxylicacid. Additionally, the divalent organic group which is free of anaromatic ring and represented e.g. by R⁴ in the structural unit (4)refers to the organic group sandwiched between NH and CO groups at thetime of ring-opening of a lactam.

The polyamide may include a copolymerized polyamide. Alternatively, thepolyamide may be a mixed polyamide, or a combination of a copolymerizedpolyamide with a mixed polyamide. Among them, a mixed polyamide ispreferred in point of improvements in mechanical strengths, notably inimpact resistance.

The copolymerized polyamide is a copolymerized polyamide obtained bycopolymerizing e.g. a polyamide having aromatic ring-containingstructural units except aramide structural units and a polyamide havingaromatic ring-free structural units.

The mixed polyamide is e.g. a mixed polyamide including an aromaticring-containing polyamide and an aromatic ring-free polyamide.

In the copolymerized polyamide, a suitable ratio by mass betweenaromatic polyamide and aliphatic polyamide (aromatic polyamide/aliphaticpolyamide) is from 20/80 to 99/1 (preferably from 50/50 to 96/4) inpoint of further improvement in mechanical strengths, notably in impactresistance.

In the mixed polyamide also, a suitable ratio by mass between aromaticpolyamide and aliphatic polyamide (aromatic polyamide/aliphaticpolyamide) is from 20/80 to 99/1 (preferably from 50/50 to 96/4) inpoint of further improvement in mechanical strengths, notably in impactresistance.

In the aromatic polyamide, a suitable proportion of aromaticring-containing structural units to all the structural units is 80 mass% or above (preferably 90 mass % or above, more preferably 100 mass %).

On the other hand, in the aliphatic polyamide, a suitable proportion ofaromatic ring-free structural units to all the structural units is 80mass % or above (preferably 90 mass % or above, more preferably 100 mass%).

Examples of the aromatic polyamide include polycondensates of aromaticring-containing dicarboxylic acids and aromatic ring-free diamines andpolycondensates of aromatic ring-free dicarboxylic acids and aromaticring-containing diamines.

Examples of the aliphatic polyamide include polycondensates of aromaticring-free dicarboxylic acids and aromatic ring-free diamines, andring-opened polycondensates of aromatic ring-free lactams.

Examples of the aromatic ring-containing dicarboxylic acid includephthalic acids (such as terephthalic acid and isophthalic acid) andbiphenyl dicarboxylic acids.

Examples of the aromatic ring-free dicarboxylic acid include oxalicacid, adipic acid, suberic acid, sebacic acid,1,4-cyclohexanedicarboxylic acid, malonic acid, succinic acid, glutaricacid, pimelic acid and azelaic acid.

Examples of the aromatic ring-containing diamine includep-phenylenediamine, m-phenylenediamine, m-xylylenediamine,diaminodiphenylmethane and diaminodiphenyl ether.

Examples of the aromatic ring-free diamine include ethylenediamine,pentamethylenediamine, hexamethylenediamine, nonanediamine,decamethylenediamine and 1,4-cyclohexanediamine.

Examples of the aromatic ring-free lactam include ε-caprolactam,undecanelactam and lauryllactam.

By the way, as each of the dicarboxylic acids, each of the diamine orthe lactam, one kind thereof may be used or two or more kinds thereofmay be used in combination.

Examples of the aromatic polyamide include MXD6 (a polycondensate ofadipic acid and m-xylylenediamine), nylon 6T (a polycondensate ofterephthalic acid and hexamethylenediamine) and nylon 9T (apolycondensate of terephthalic acid and nonanediamine).

Examples of a commercially available aromatic polyamide product includeMXD6 produced by Mitsubishi Gas Chemical Industry, Inc., Genestar®:PA6T, produced by KURARAY CO., LTD., Genstar®: PA9T, produced by KURARAYCO., LTD., and TY-502NZ: PA6T, produced by TOYOBO CO., LTD.

Examples of the aliphatic polyamide include nylon 6 (ring-openedpolycondensate of ε-caprolactam), nylon 11 (ring-opened polycondensateof undecanelactam), nylon 12 (ring-opened polycondensate oflauryllactam), nylon 66 (polycondensate of adipic acid andhexamethylenediamine), nylon 610 (polycondensate of sebacic acid andhexamethylenediamine) and nylon 612 (polycondensate of caprolactum(carbon number: 6) and lauryllactam (carbon number: 12).

Examples of a commercially available aliphatic polyamide product includeZytel®: 7331J (PA6), produced by Du Pont and Zytel®: 101L (PA66),produced by Du Pont.

The proportion of aromatic rings in a polyamide (a copolymerizedpolyamide or a mixed polyamide) is preferably from 1 mass % to 55 mass%, more preferably from 5 mass % to 50 mass %, still more preferablyfrom 10 mass % to 40 mass %, in point of further enhancement ofmechanical strengths, notably bending elasticity modulus.

By the way, the proportion of aromatic rings in a mixed polyamide istaken as a proportion of aromatic rings in the total for aromaticpolyamides and aliphatic polyamides.

The wording “the proportion of aromatic rings in a polyamide” usedherein refers to the proportion of the total for monocyclic aromaticrings and fused rings produced by fusing together monocyclic aromaticrings. In calculating the proportion of aromatic rings in a polyamide,substituents attached to monocyclic aromatic rings and fused ringsproduced by fusing together monocyclic aromatic rings are excluded.

In other words, the proportion of aromatic rings in a polyamide isdetermined from calculation of the molecular weight of a structural unitproduced by polycondensation of a dicarboxylic acid and a diamine or themolecular weight of a structural unit produced by ring-opening of alactam and calculation of the proportion (mass %) of molecular weight ofaromatic rings (aromatic rings after removing substituents therefrom inthe case of having substituents) present in such a structural unit tothe molecular weight of the structural unit containing the aromaticrings.

Then, proportions of aromatic rings in representative polyamides aregiven below. The proportions of aromatic rings in nylon 6 and nylon 66which have no aromatic rings are both 0 mass %. On the other hand, inthe case of MXD6 having aro:matte rings, the proportion of aromaticrings is 30.9 mass % because it has an aromatic ring —C₆H₄— (molecularweight: 76.10) in each individual structural unit. Likewise, in the caseof nylon 9T, the proportion of aromatic rings is 26.4 mass %.

-   6 Nylon 6: Structural unit with formula [—NH—(CH₂)₅—CO—], molecular    weight of structural unit=113.16, proportion of aromatic rings=0    mass %-   Nylon 66: Structural unit with formula    [—NH—(CH₂)₆—NH—CO—(CH₂)₄—CO—], molecular weight of structural    unit=226.32, proportion of aromatic rings=0 mass %-   MXD6: Structural unit with formula    [—NH—CH₂—C₆H₄—CH₂—NH—CO—(CH₂)₄—CO—], molecular weight of structural    unit=246.34, proportion of aromatic rings=30.9 mass %-   Nylon 9T: Structural unit with formula [—NH—(CH₂)₉—NH—CO—C₆H₄—CO—],    molecular weight of structural unit=288.43, proportion of aromatic    rings=26.4 mass %

And the proportions of aromatic rings in a copolymerized polyamide and amixed polyamide are determined as follows.

—Case 1: Copolymerized Polyamide or Mixed Polyamide of Nylon 6 and MXD6(Nylon 6/MXD6 Ratio by Mass=50/50)—

Proportion of aromatic rings=(proportion of nylon 6×proportion ofaromatic rings in nylon 6)+(proportion of MXD6×proportion of aromaticrings in MXD6) (0.5×0)=(0.5×30.9)=15.5 (mass %)

—Case 2: Copolymerized Polyamide or Mixed Polyamide of Nylon 66, MXD6and Nylon 9T (Nylon 66/MXD6/Nylon 9T Ratio by Mass=50/25/25)—

Proportion of aromatic rings=(proportion of nylon 66×proportion ofaromatic rings in nylon 66)+(proportion of MXD6×proportion of aromaticrings in MXD6)+(proportion of nylon 9T×proportion of aromatic rings innylon 9T)=(0.5×0)+(0.25×30.9)+(0.25×26.4)=14.35 (mass %)

Physical properties of polyamide are explained below.

The molecular weight of polyamide is not particularly limited so long asit allows easier hot-melt of the polyamide than hot-melt of polyolefinpresent together in the resin composition. For example, it isappropriate that the weight-average molecular weight of polyamide befrom 10,000 to 300,000, preferably from 10,000 to 100,000.

In addition, the glass transition temperature or melting temperature(melting point) of polyamide is not particularly limited as is the casewith the molecular weight so long as it allows easier hot-melt of thepolyamide than hot-melt of polyolefin present together in the resincomposition. For example, it is appropriate that the melting temperature(Tm) of each polyamide be in a range of 100° C. to 400° C., preferablyin a range of 150° C. to 350° C.

By the way, the melting temperature (Tm) of polyamide is determined bythe same method as adopted in the foregoing melting temperaturemeasurement made on polyolefin. To be more specific, the meltingtemperature (Tm) of polyamide is determined from the DSC curve obtainedby differential scanning calorimetry (DSC) as “melting peak temperature”described in JIS K 71214987, directions for determination of meltingtemperature in “methods for measuring transition temperature ofplastic”.

—Carboxylic Anhydride-Modified Polyolefin Compatibilizer—

The compatibilizer is a resin allowing enhancement of an affinitybetween polyolefin and polyamide.

The compatibilizer may be chosen in response to the polyolefin usedtogether.

As the compatibilizer, it is appropriate to use carboxylicanhydride-modified polyolefin which has the same structure as thepolyolefin used together and contains, in portions of its molecule,moieties having an affinity for polyamide.

The carboxylic anhydride-modified polyolefin is a modified polyolefinhaving portions into which moieties containing carboxylic anhydrideresidues are introduced.

For example, when the polyolefin is polypropylene (PP), the modifiedpolyolefin is preferably a modified polypropylene (PP), while when thepolyolefin is an ethylene-vinyl acetate copolymer resin (EVA), themodified polyolefin is preferably a modified ethylene-vinyl acetatecopolymer resin (EVA).

As the modifying moiety which contains a carboxylic anhydride residueand is introduced into a polyolefin, a maleic anhydride residue inparticular is suitable in point of further enhancement of an affinitybetween polyolefin and polyamide, and besides in point of the upperlimit of temperature during the molding process.

As a method for producing a modified polyolefin, there are e.g. a methodof directly forming chemical bonds by making the foregoing compoundhaving a modifying moiety react with a polyolefin, and a method offorming graft chains by the use of the foregoing compound having amodifying moiety, then making the graft chains combine with apolyolefin.

Examples of the foregoing compound containing a modifying moiety includemaleic anhydride and citric anhydride and derivatives of theseanhydrides.

Of the above compatibilizers, a maleic anhydride-modified polyolefinproduced by making maleic anhydride as an unsaturated carboxylic acidreact with a polyolefin is preferred over the others.

Examples of a modified polyolefin include maleic anhydride-modifiedpolypropylene, maleic anhydride-modified polyethylene, maleicanhydride-modified ethylene-vinyl acetate copolymer resin (EVA), and anacid-modified polyolefin such as an addition product or copolymer ofthose recited above. When the polyolefin is polypropylene, maleicanhydride-modified polypropylene is especially preferred.

As the modified polyolefin, commercially available products may be used.

Examples of a commercially available modified polypropylene includeUMEX® series (e.g. 100TS, 110TS, 1001, 1010) produced by Sanyo ChemicalIndustries, Ltd.

Examples of a commercially available modified polyethylene include UMEX®series (e.g. 2000) produced by Sanyo Chemical Industries, Ltd., and aMODIC® series produced by Mitsubishi Chemical Corporation.

Examples of a commercially available modified ethylene-vinyl acetatecopolymer resin (EVA) include a MODIC® series produced by MitsubishiChemical Corporation.

By the way, the molecular weight of a compatibilizer has no particularlimits, but in melt-fabricable point of view, it is preferably in arange of 5,000 to 100,000, more preferably in a range of 5,000 to80,000.

—Other Ingredients—

The resin composition relating to an embodiment of the invention mayfurther contain ingredients other than those mentioned above.

Examples of other ingredients include well-known additives such as aflame retardant, a flame retarding assistant, an agent for inhibitingdrips during heating (a drip inhibitor), a plasticizer, an antioxidant,a release agent, a lightfastness agent, a weatherproof agent, a coloringagent, pigments, a modifier, an antistatic agent, a hydrolysisinhibitor, a filler and a reinforcing agent other than carbon fibers(e.g. talc, clay, mica, glass flakes, milled glass, glass beads,crystalline silica, alumina, silicon nitride, aluminum nitride, boronnitride or so on).

In addition to carbon fibers, other fibrous reinforcing materials may beincorporated.

The other fibrous reinforcing materials have no particular restrictionsso long as they are fibrous in form. Examples of a fibrous reinforcingmaterial include continuous or discontinuous reinforced fibers such asglass fiber, aramide fiber, silicon carbide fiber, alumina fiber, boronfiber, tungsten carbide fiber and organic fibers (e.g. aramide, vinylon,nylon and cellulose fibers). Where fiber-reinforced fillers areconcerned also, only one kind thereof may be added, or two or more kindsthereof may be added in combination.

The size of a fibrous reinforcing material has no particular limits. Itis appropriate for the fibrous reinforcing material to have e.g. anumber-average fiber length in a range of 20 μm to 40 mm, preferably ina range of 30 μm to 30 mm. In addition, it is appropriate for thefibrous reinforcing material to have a number-average fiber diameter ina range of 1 μm to 30 μm, preferably in a range of 1 μm to 20 μm. By theway, it is adequate that a reinforcing material in a raw material statebefore undergoing melt-kneading with a thermoplastic resin or the likemeets requirements that its number-average fiber length and itsnumber-average fiber diameter be in the respective ranges specifiedabove, and it is preferred that the reinforcing material meet suchrequirements even after undergoing melt-kneading.

It is appropriate for the foregoing other ingredients to be added e.g.in an amount of 0 parts by mass to 10 parts by mass, preferably in anamount of 0 parts by mass to 5 parts by mass, with respect to 100 partsby mass of polyolefin. The expression “0 parts by mass” herein means astate that no other ingredients are incorporated.

<Resin Molding>

A resin molding relating to an embodiment of the invention contains apolyolefin, a polyamide, carbon fibers and a compatibilizer. In otherwords, the resin molding relating to an embodiment of the invention isconstituted of the same ingredients that constitute the resincomposition relating to an embodiment of the invention.

More specifically, the present resin molding contains, with respect to100 parts by mass of a polyolefin, 1 part by mass to 50 parts by mass ofa polyamide, 1 part by mass to 50 parts by mass of carbon fibers havingan average fiber length of 0.2 mm to 1 mm and including carbon fibershaving their fiber lengths in a range of 1 mm to 20 mm in a proportionof 1% to 20% by number to all the carbon fibers, and 1 part by mass to10 parts by mass of a carboxylic anhydride-modified polyolefin as acompatibilizer.

In other words, the resin molding contains a polyolefin, and furthercontains, per 100 parts by mass of polyolefin, a polyamide in a contentof 1 part by mass to 50 parts by mass, carbon fibers in a content of 1part by mass to 50 parts by mass and a compatibilizer in a content of 1part by mass to 10 parts by mass.

And the carbon fibers have an average fiber length in a range of 0.2 mmto 1 mm, and the percentage by number of the carbon fibers from 1 mm to20 mm in fiber length to all the carbon fibers is from 1% to 20%.

In addition, the percentage by number of the carbon fibers from 1 mm to20 mm in fiber length to all the carbon fibers is preferably from 5% to20% from the viewpoint of enhancing impact resistance.

By the way, it is appropriate for the resin molding relating to anembodiment of the invention to be a non-crosslinked resin molding.

The resin molding relating to an embodiment of the invention may be onewhich is obtained by preparing a resin composition relating to anembodiment of the invention, and then molding this resin composition. Inproducing a resin molding relating to an embodiment of the invention bymolding a resin composition relating to an embodiment of the invention,the carbon fibers included in the resin molding are in a mixed state offirst carbon fibers and second carbon fibers.

Herein, the carbon fiber content represents the whole quantity of carbonfibers included in the resin molding, and the average fiber length ofcarbon fibers represents an average fiber length of all the carbonfibers included in the resin molding. In addition, the proportion bynumber of carbon fibers having their fiber lengths in a range of 1 mm to20 mm is expressed in terms of the percentage by number to all thecarbon fibers included in the resin molding.

The method for measuring an average length of fibers included in themolding is as described already. In addition, the proportion by numberof carbon fibers having their fiber lengths in a range of 1 mm to 20 mmis determined by performing image analysis according to the methoddescribed already and checking for the number of carbon fibers bayingtheir fiber lengths in a range of 1 mm to 20 mm among all the carbonfibers on which average fiber-length measurement have been made.

Examples of a method applicable to forming of a resin molding relatingto an embodiment of the invention include injection molding, extrusionmolding, blow molding, hot press molding, calender molding, coatingmolding, cast molding, dipping molding, vacuum molding and transfermolding.

The method for forming the resin molding relating to an embodiment ofthe invention is preferably injection molding in point of high degree offreedom in shaping.

The cylinder temperature in injection molding is e.g. from 180° C. to300° C., preferably from 200° C. to 280° C. The mold temperature ininjection molding is e.g. from 30° C. to 100° C., preferably from 30′C.to 60° C.

The injection molding may be carried out using a commercially availablemachine, such as NEX150 made by NISSET PLASTIC INDUSTRIAL CO., LTD.,NEX300 made by NISSEI PLASTIC INDUSTRIAL CO., LTD., or SE50D made bySumitomo Heavy Industries, Ltd.

The resin molding relating to an embodiment of the invention are usedsuitably for application to electrical-electronic instruments, officeinstruments, household electric appliances, car's interior materials,containers or so on. More specifically, they are used for cabinets ofelectrical-electronic instruments and household electric appliances,various parts of electrical-electronic instruments and householdelectric appliances, car's interior parts, storage cases for CD-ROM, DVDand the like, tableware, beverage bottles, food trays, wrappingmaterials, film, tarpaulin and so on.

The resin molding relating to an embodiment of the invention inparticular is a resin molding superior in mechanical strengths, notablyin bending elasticity modulus, because carbon fibers are adopted asreinforcing fibers, and hence it is used suitably as substitutes formetallic parts.

EXAMPLES

The invention will now be illustrated in more detail by reference to thefollowing examples, but these examples should not be construed aslimiting the invention in any way.

Examples 1 to 13 and Comparative Examples 1 to 11 (Preparation for ResinComposition)

Each of pellets A-1 to A-8 as the first resin compositions was preparedby kneading a set of ingredients as shown in Table 4 under kneadingconditions described below and a melt-kneading temperature (cylindertemperature) as indicated in Table 1 by means of a twin-screw kneader(TEM58SS, made by TOSHIBA MACHINE CO., LTD.) incorporating a low-shearscrew having a compression ratio of 1.8 and one pin-type mixing sectionin its screw structure.

By the way, the carbon fibers used for preparation of the pellets A-1 toA-8 were as follows.

(TORAYCA®, produced by Toray Industries, Inc., chopped carbon fibershaving undergone surface treatment, average fiber length: 20 mm, averagefiber diameter: 7 μm)

A pellet B-1 was prepared as a second resin composition containinglong-length aramide fibers through the use of PLASTRON PP-AF-30-T3 (L6)(produced by Daicel Polymer, Ltd.).

A pellet B-2 was prepared as a second resin composition containinglong-length vinylon fibers through the use of Centerfill Vinylon 30(produced by Chuo Kaseihin Co., Inc.)

A pellet B-3 was prepared by processing the pellet B-1 under thekneading conditions mentioned above to shorten the fiber length of thearamide fibers.

Further, a resin composition B-4 was prepared by mixing 70 parts of a PP(polypropylene) pellet and 30 parts of chopped aramide fibers having afiber length of 50 mm. Likewise, a resin composition A-9 was prepared bymixing 55 parts of a PP pellet, 20 parts of a PA6 pellet, 5 parts of aMA-PP pellet and 20 parts of 11 mm-length CF fibers.

A pellet B-5 was prepared as a second resin composition containing 20mm-length aramide fibers through the use of PLASTRON PP-AF-30-T3 (L20)(produced by Daicel Polymer, Ltd.).

Additionally, average fiber-length measurement of carbon fibers was madeon each of the pellets A-1 to A-9 and average fiber length measurementof organic fibers was made on each of the pellets B-1 to B-5 inaccordance with the method described already. Results of themeasurements are shown in Table 1.

TABLE 1 Manufacturing Example No. 1 2 3 4 5 6 7 8 9 — — 10 11 12 PelletNo. A-1 A-2 A-3 A-4 A-5 A-6 A-7 A-8 A-9 B-1 B-2 B-3 B-4 B-5 IngredientPP 55 60 55 57 60 60 55 70 70 70 70 70 content PE 55 (parts by EVA 55mass) PA6 30 15 10 10 10 10 20 PA66 20 MXD6 20 10 MA-PP 5 5 5 8 5 3 5MA-PE 5 MA-EVA 5 Carbon fiber 10 20 30 15 15 17 30 30 20 Organic fiber30 30 30 30 30 Total 100 100 100 100 100 100 100 100 100 100 100 100 100100 Melt-kneading temperature 240 240 240 270 240 240 240 240 — — — 180— — Average fiber-length of carbon fibers (mm) 0.5 0.5 0.5 0.3 0.8 0.80.5 0.5 11 — — — — — Average fiber-length of organic fibers (mm) 6 120.9 50 20 Note Polyamide content 55 25 18 35 33 33 18 18 36 0 0 0 0 0(per 100 parts of PO) Compatibilizer content 9 8 9 14 8 5 9 9 9 0 0 0 00 (per 100 parts of PO) Carbon fiber content 18 33 55 26 25 28 55 55 360 0 0 0 0 (per 100 parts of PO) Organic fiber content 0 0 0 0 0 0 0 0 043 43 43 43 43 (per 100 parts of PO)

(Injection Molding)

Each of the pellets A-1 to A-9 and each of the pellets B-1 to B-5 weremixed together according to the formula as shown in Table 2 or Table 3,and molded into an ISO multipurpose dumbbell test piece (compliant withISO 527 tensile test and ISO 178 bending test) (test part thickness 4mm, width 10 mm) and a D2 test piece (length 60 mm, width 60 mm,thickness 2 mm) by using an injection molding machine (NEX150, made byNISSEI PLASTIC INDUSTRIAL. CO., LTD.) at a cylinder temperature asindicated in Table 5 or Table 6 and a mold temperature 50° C. under aback pressure of 10 MPa.

<Evaluations>

By using the two kinds of test pieces thus formed, the followingevaluations were made. Evaluation results obtained are shown in Table 2and Table 3.

(Analyses of Carbon Fibers and Organic Fibers)

The average fiber length of carbon fibers, the average fiber length oforganic fibers and the percentage by number of fibers from 1 mm to 20 mmin fiber length to the total for carbon fibers and organic fibers(hereafter expressed as “percentage of fibers at least 1 mm in length”)were measured according to the already-described methods, respectively.

(Moldability in Forming Resin Molding)

Moldability of each resin composition was evaluated as follows.

After forming a resin pellet from each of the compositions prepared soas to have ingredient contents according to Table 2 or Table 3, a 4mm-thick multipurpose test piece A1 conforming to JIS K7139 was moldedinto a dumbbell sample by means of an injection molding machine.

—Evaluation Criteria—

A: Molding defects including unevenness, defective part and the like arenot observed in all area of the molded surface, namely the moldedsurface is uniform.

B: Molding defects including unevenness, defective part and the like aredeveloped in an area smaller than 20% of the molded surface.

C: Molding defects including unevenness, defective part and the like aredeveloped in an area larger than or equal to 20% of the molded surface.

(Bending Elasticity Modulus)

Bending elasticity modulus measurements were made on each of theforegoing ISO multipurpose dumbbell test pieces by using a methodconforming to ISO178 and universal testing apparatus (AutographAG-Xplus, made by SHIMADZU CORPORATION).

(Impact Resistance)

Each of the foregoing ISO multipurpose dumbbell test pieces wassubjected to notching (4 mm in plate thickness), and its Charpy impactstrength (kJ/m²) was measured by conforming to the method defined in ISO179 and using an impact testing instrument (DG-5, made by Toyo SeikiSeisaku-Sho, Ltd.), The greater the measured value, the higher theimpact resisting strength.

(Presence or Absence of Covering Layer)

Each of the foregoing D2 test pieces was checked up on the presence orabsence of a covering layer of polyamide in accordance with the methoddescribed already.

TABLE 2 Example No. 1 2 3 4 5 6 7 Mixed Ingredient A-1 90 85 PelletContent A-2 90 (parts by A-3 85 70 mass) A-4 75 A-5 80 A-6 A-7 A-8 A-9B-1 10 10 15 15 30 25 20 B-2 B-3 B-4 B-5 Total 100 100 100 100 100 100100 Carbon fiber content 9 16 25.5 8.5 21 11.25 12 CF1 (parts by mass)Organic fiber content 3 3 4.5 4.5 9 7.5 8 OF2 (parts by mass) Fiberratio (CF1/OF2) 75/25 86/14 85/15 65/35 70/30 60/40 67/33 ResinIngredient PP 56.5 61 57.25 57.25 59.5 60.25 62 Molding Content PE(parts by EVA mass) PA6 27 13.5 8.5 25.5 7 PA66 15 MXD6 15 MA-PP 4.5 4.54.25 4.25 3.5 6 4 MA-PE MA-EVA Carbon fibers 9 16 25.5 8.5 21 11.25 12Organic fibers 3 5 4.5 4.5 9 7.5 6 Total 100 100 100 100 100 100 100Molding temperature 240 240 240 240 240 270 240 (cylinder temperature °C.) Average fiber length of 0.3 0.3 0.3 0.3 0.3 0.2 0.4 carbon fibers(mm) Average fiber length of 3 3 3 5 3 4 4 organic fibers (mm)Percentage of fibers at least 18 10 4 18 6 8 12 1 mm in length (number%) Property Moldability in forming A A A A A A A resin molding Bendingelasticity 10 15 20 8 18 12 12 modulus (Gpa) Charpy (kJ/m²) 15 11 9 1612 11 11 Presence or absence Presence Presence Presence PresencePresence Presence Presence of covering layer Note Polyamide content 47.522.1 14.8 44.5 11.8 24.9 25.8 (per 100 parts of PO) Compatibilizercontent 8 7.4 7.4 7.4 5.9 10 6.5 (per 100 parts of PO) Carbon fibercontent 15.9 29.5 44.5 14.8 35.9 18.7 18.4 (per 100 parts of PO) Organicfiber content 5.3 4.9 7.9 7.9 15.1 12.4 9.7 (per 100 parts of PO)Example No. 8 9 10 11 12 13 Mixed Ingredient A-1 75 Pellet Content A-290 (parts by A-3 mass) A-4 A-5 A-6 80 80 A-7 90 A-8 90 A-9 B-1 20 10 10B-2 25 20 B-3 B-4 B-5 10 Total 100 100 100 100 100 100 Carbon fibercontent 13.6 7.5 13.6 27 27 18 CF1 (parts by mass) Organic fiber content6 7.5 6 3 3 3 OF2 (parts by mass) Fiber ratio (CF1/OF2) 69/31 50/5069/31 90/10 90/10 86/14 Resin Ingredient PP 62 58.75 62 7 7 61 MoldingContent PE 49.5 (parts by EVA 49.5 mass) PA6 8 22.5 8 9 9 13.5 PA66 MXD68 8 MA-PP 2.4 3.75 2.4 4.5 MA-PE 4.5 MA-EVA 4.5 Carbon fibers 13.6 7.513.6 27 27 18 Organic fibers 6 7.5 6 3 3 3 Total 100 100 100 100 100 100Molding temperature 240 240 240 240 240 240 (cylinder temperature ° C.)Average fiber length of 0.4 0.4 0.4 0.3 0.3 0.3 carbon fibers (mm)Average fiber length of 4 2 1 3 3 18 organic fibers (mm) Percentage offibers at least 10 3 2 4 4 12 1 mm in length (number %) PropertyMoldability in forming A A A A A A resin molding Bending elasticity 1310 15 12 10 12 modulus (Gpa) Charpy (kJ/m²) 10 15 16 14 16 20 Presenceor absence Presence Presence Presence Presence Presence Presence ofcovering layer Note Polyamide content 25.8 38.3 25.5 15.9 15.9 22.1 (per100 parts of PO) Compatibilizer content 3.9 6.4 3.9 6 8 7.4 (per 100parts of PO) Carbon fiber content 21.8 12.8 21.9 47.8 47.8 29.5 (per 100parts of PO) Organic fiber content 9.7 12.8 9.7 6.3 5.3 4.9 (per 100parts of PO)

TABLE 3 Comparative Example No. 1 2 3 4 5 6 Mixed Ingredient A-1 100 95pellet content A-2 35 (parts by A-3 97 mass) A-4 95 A-5 A-6 A-7 A-8 A-9B-1 100 3 65 5 5 B-2 B-3 B-4 B-5 Total 100 100 100 100 100 100 Carbonfiber content 10 0 29.1 7 9.5 14.25 CF1 (parts by mass) Organic fibercontent 0 30 0.9 19.5 1.5 1.5 OF2 (parts by mass) Fiber ratio (CF1/OF2)100/0 0/100 97/3 26/74 86/14 90/10 Resin Ingredient PP 55 70 55.45 66.555.75 57.65 Molding Content PE (parts by EVA mass) PA6 30 9.7 5.25 28.5PA66 19 MXD6 MA-PP 5 4.85 1.75 4.75 7.6 MA-PE MA-EVA Carbon fibers 1029.1 7 9.5 14.25 Organic fibers 30 0.9 19.5 1.5 1.5 Total 100 100 100100 100 100 Molding temperature 240 180 240 240 240 270 (Cylindertemperature ° C.) Average fiber length of 0.3 — 0.3 0.3 0.3 0.2 carbonfibers (mm) Average fiber length of — 6 3 3 4 4 organic fibers (mm)Percentage of fibers at least 0 100 3 30 4 4 1 mm in length (number %)Property Moldability in forming A B A B A A resin molding Bendingelasticity 14 5 12 6 6 13 modulus (Gpa) Charpy (kJ/m²) 6 18 7 12 6 6Presence or absence Presence Presence Presence Presence PresencePresence of covering Note Polyamide content 54.5 0 17.5 7.9 51.1 33 (per100 parts of PO) Compatibilizer content 9.1 0 8.7 2.6 8.5 13.2 (per 100parts of PO) Carbon fiber content 18.2 0 52.6 10.5 17 24.7 (per 100parts of PO) Organic fiber content 0 42.9 1.6 29.3 2.7 2.6 (per 100parts of PO) Comparative Example No. 7 8 9 10 11 Mixed Ingredient A-1pellet content A-2 95 95 (parts by A-3 mass) A-4 A-5 A-6 A-7 100 A-8 100A-9 95 B-1 5 B-2 B-3 5 B-4 5 B-5 Total 100 100 100 100 100 Carbon fibercontent 30 30 19 19 19 CF1 (parts by mass) Organic fiber content 0 0 1.51.5 1.5 OF2 (parts by mass) Fiber ratio (CF1/OF2) 100/0 100/0 93/7 93/793/7 Resin Ingredient PP 60.5 60.5 55.75 Molding Content PE 55 (parts byEVA 55 mass) PA6 10 10 14.25 14.25 19 PA66 MXD6 MA-PP 4.75 4.75 4.75MA-PE 5 MA-EVA 5 Carbon fibers 30 30 19 19 19 Organic fibers 1.5 1.5 1.5Total 100 100 100 100 100 Molding temperature 240 240 270 240 240(Cylinder temp. ° C.) Average fiber length of 0.3 0.3 0.2 0.4 3 carbonfibers (mm) Average fiber length of — — 0.5 25 4 organic fibers (mm)Percentage of fibers at least 0 0 0.7 4 60 1 mm in length (number %)Property Moldability in forming A A A C C resin molding Bendingelasticity 9 8 5 8 14 modulus (Gpa) Charpy (kJ/m²) 7 8 8 15 6 Presenceor absence Presence Presence Presence Presence Presence of covering NotePolyamide content 18.2 18.2 23.6 23.6 34.1 (per 100 parts of PO)Compatibilizer content 9.1 9.1 7.9 7.9 8.6 (per 100 parts of PO) Carbonfiber content 54.5 54.5 31.4 31.4 34.1 (per 100 parts of PO) Organicfiber content — — 2.5 2.5 2.7 (per 100 parts of PO)

The wording “content (per 100 parts of PO)” in the note column refers toa content expressed in parts by mass with respect to 100 parts by massof polyolefin.

Details of the kinds of ingredients in Table 1 to Table 3 are asfollows.

—Polyolefin—

PP: Polypropylene (NOVATEC® PPMA3, produced by Japan PolypropyleneCorporation)

PE: Polyethylene (ULTZEX® 20100J, produced by Prime Polymer Co., Ltd.)

EVA: Ethylene-vinyl acetate copolymer resin (41XEV250, produced by DUPONT-MITSUI POLYCHEMICALS CO., LTD.)

—Polyamide: Aliphatic PA (aliphatic polyamide)—

PA6: (Nylon 6 Zytel® 7331J, produced by Du Pont, melting temperature:225° C.)

PA66: (Nylon 66 101L, produced by Du Pont, melting temperature: 260° C.)

—Polyamide: Aromatic PA (aromatic polyamide)—

MXD6: (MXD6 produced by MITSUBISHI GAS CHEMICAL COMPANY, INC., meltingtemperature: 237° C.)

—Compatibilizer—

MA-PP: Maleic anhydride-modified polypropylene (UMEX® 110TS, produced bySanyo Chemical Industries, Ltd.)

MA-PE: Maleic anhydride-modified polyethylene (MODIC® M142, produced byMitsubishi Chemical Corporation)

MA-EVA: Maleic anhydride-modified ethylene-vinyl acetate copolymer resin(MODIC® A543, produced by Mitsubishi Chemical Corporation)

As can be seen from the data shown above, results of impact resistingstrength evaluations made on Examples are better than those made onComparative Examples.

In addition, by analyzing each of the moldings produced in Examples inaccordance with the method described already, it has been ascertainedthat there was an intervening layer of the compatibilizer used (a layerof maleic anhydride-modified polypropylene, maleic anhydride-modifiedpolyethylene or maleic anhydride-modified ethylene-vinyl acetatecopolymer resin (EVA)) between the covering layer and the polyolefin (orequivalently, a layer of compatibilizer was formed on the coveringlayer's surface).

What is claimed is:
 1. A resin molding comprising: a polyolefin; apolyamide in a content of 1 part by mass to 50 parts by mass per 100parts of the polyolefin; carbon fibers in a content of 1 part by mass to50 parts by mass per 100 parts by mass of the polyolefin; organic fibersin a content of 1 part by mass to 20 parts by mass per 100 parts by massof the polyolefin, the organic fibers having an average fiber length of1 mm to 20 mm; and a carboxylic anhydride-modified polyolefin as acompatibilizer in a content of 1 part by mass to 10 parts by mass per100 parts by mass of the polyolefin, wherein a proportion of a carbonfiber and an organic fiber each having a fiber length in a range of 1 mmto 20 mm to all the carbon fibers and the organic fibers is 1% to 20% bynumber.
 2. The resin molding according to claim 1, wherein thepolyolefin is at least one selected from the group consisting ofpolypropylene, polyethylene, and ethylene-vinyl acetate copolymer. 3.The resin molding according to claim 1, wherein the compatibilizer is atleast one modified polyolefin selected from the group consisting of amodified polypropylene, a modified polyethylene, and a modifiedethylene-vinyl acetate copolymer, and the modified polyolefin has amodified moiety containing a carboxylic anhydride residue.
 4. The resinmolding according to claim 3, wherein the carboxylic anhydride residueis a maleic anhydride residue.
 5. The resin molding according to claim1, wherein the organic fibers have a melting point higher than a meltingpoint of polyolefin, a softening point higher than the melting point ofpolyolefin, or a thermal decomposition temperature higher than themelting point of polyolefin.
 6. The resin molding according to claim 5,wherein the organic fibers are at least one of aramid fibers and vinylonfibers.
 7. The resin molding according to claim 1, wherein part of thepolyamide forms a covering layer around the periphery of each of thecarbon fibers.
 8. The resin molding according to claim 7, wherein thecompatibilizer forms an intervening layer between the covering layer andthe polyolefin.
 9. The resin molding according to claim 1, which is anon-crosslinked resin molding.
 10. The resin moldings according to claim1, the content of the polyamide is from 11.8 parts by mass to 50 partsby mass, and the content of the compatibilizer is from 3.9 parts by massto 10 parts by mass.